When the reservoir pressure and temperature of a supersonic wind tunnel are (15 mathrm{~atm}) and (750 mathrm{~K}),
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When the reservoir pressure and temperature of a supersonic wind tunnel are \(15 \mathrm{~atm}\) and \(750 \mathrm{~K}\), respectively, the mass flow is \(1.5 \mathrm{~kg} / \mathrm{s}\). If the reservoir conditions are changed to \(p_{o}=20 \mathrm{~atm}\) and \(T_{o}=600 \mathrm{~K}\), calculate the mass flow.
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